N451KT
Raytheon Premier I (Model 390) (Premier I)
Raytheon Aircraft Company
3 Hours
Duration of Flight
1350 NM
Range
451 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2025-11-26No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Raytheon Premier I (Model 390) (Premier I)
Overview
Registered to DAWSON AERO LLC, Fayetteville, AR. Model 390 (Raytheon Premier I), MSN RB-74, MFR Year 2003. FAA certificate issued 2025-06-03; registration expiration 2032-06-30. Status: Valid.
Specifications
- Engines: 2× Williams FJ44-2A (2300 lbf each)
- Range: 1350 nm
- Cruise: 451 kts
- Seats: 6
- Ceiling: 41000 ft
Operations & Cabin
Standard 6-place executive (club 4 + 2 forward-facing) with rear lavatory; single-pilot capable Six-place executive layout, swiveling/reclining club seats, stowable tables, forward and aft baggage compartments, rear lavatory Avionics: Rockwell Collins Pro Line 21 (typical)
Model & Market Context
This entry covers airframe N451KT, a Raytheon Premier I (Model 390) built in 2003 with manufacturer serial number RB-74. The airframe is registered in the United States and is owned by DAWSON AERO LLC, an LLC based in Fayetteville, AR, United States; the current ownership is notable as a single-corporate operator responsible for the aircraft’s civil registry and operational oversight. The Premier I was delivered as a light business jet and has been maintained to the standard specification for the type; ownership by DAWSON AERO LLC represents the latest documented operator record for this tail number. Public valuation or condition ratings specific to this airframe are not published in the supplied data.
The cabin of N451KT is fitted in the standard six-place executive configuration (club four plus two forward-facing) with a rear lavatory and is certified for single-pilot operation, providing operational flexibility for owner-operators or charter missions. Avionics are typical for the type, with a Rockwell Collins Pro Line 21 suite specified as the common fit; this supports modern IFR operations, integrated flight management, and situational awareness for single-pilot dispatch. Based in Fayetteville, AR, the aircraft’s performance—particularly its high cruise speed and regional range—suits point-to-point business travel across the continental United States and short international hops from domestic bases. Routine maintenance considerations for this airframe align with the Premier I fleet norms, focusing on its composite nose and wing structures and Williams turbofan engine program requirements.
The Raytheon Premier I (Model 390) occupies the light, high-speed business jet niche, offering transcontinental short-haul capability with a cruising speed around 451 kts and a service ceiling near 41,000 ft. Competing models in the class include other light jets that target six-passenger corporate missions; demand often comes from owner-operators, small charter operators, and corporate flight departments seeking high speed and cabin comfort in a compact airframe. From a maintenance and resale perspective, buyers consider the Williams FJ44 engine maintenance program, avionics configuration such as Pro Line 21, single-pilot capability, and the airframe’s entry age (built 2003) when evaluating lifecycle costs and market value.
Aircraft Comparison
| Parameter | N451KT | N100HL | N100WE |
|---|---|---|---|
| Serial Number (MSN) | RB-74 | 258345 | RB-45 |
| Year Manufactured | 2003 | 1997 | 2002 |
| Duration of Flight | 3 Hours | 6 Hours | 3 Hours |
| Range | 1350 NM | 2470 NM | 1460 NM |
| Max Speed | 451 MPH | 447 MPH | 454 MPH |
| Aircraft Class | 12,500 lbs (MTOW) | Over 20,000lbs | 12,500-19,999lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 6 | 8 | 8 |
| Cabin Comfort | No items found. | No items found. | No items found. |